View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 48274U 21035A 22146.07082191 .00028824 00000-0 34676-3 0 9992
2 48274 41.4728 353.3761 0002014 59.2290 78.9210 15.60193327 61310
| Epoch (UTC): | 26 May 2022 01:41:59 |
| Eccentricity: | 0.0002014 |
| inclination: | 41.4728° |
| perigee height: | 386 km |
| apogee height: | 388 km |
| right ascension of ascending node: | 353.3761° |
| argument of perigee: | 59.2290° |
| revolutions per day: | 15.60193327 |
| mean anomaly at epoch: | 78.9210° |
| orbit number at epoch: | 6131 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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